Results 131 to 140 of about 102,092 (253)
Effect of a simulated engine jet blowing above an arrow wing at Mach 2.0 [PDF]
The effects of a gas jet simulating a turbojet engine exhaust blowing above a cambered and twisted arrow wing were investigated. Tests were conducted in the Langley 4-foot supersonic pressure tunnel at a Mach number of 2.0.
Hayes, C., Shrout, B. L.
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Arthritis &Rheumatology, Accepted Article.Objectives The unknown pathophysiology and the lack of specific features for systemic Juvenile Idiopathic arthritis and adult‐onset Still disease (collectively Still disease/SD) delays diagnosis and appropriate treatment. The goal of this study was to identify features and mechanisms that distinguish SD from other systemic autoinflammatory diseases ...
Yvonne M. Mueller +17 more
wiley +1 more source
Flow visualization of discrete hole film cooling for gas turbine applications [PDF]
Film injection from discrete holes in a three row staggered array with 5-diameter spacing is studied. The boundary layer thickness-to-hole diameter ratio and Reynolds number are typical of gas turbine film cooling applications.
Colladay, R. S., Russell, L. M.
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Numerical Simulation of Molten Steel Flow in Tundish with Gas Curtain
Teshugang, 2006 Based on operation process parameters of tundish for two strand concasting 1500 mmx 250 mm slab,using Eulerian multiphase model,porous media model and Larangian random-trajectory model,the characteristics of molten steel flow and inclusion moving trace ...
张美杰 +4 more
doaj
Augmentation of Fighter-Aircraft Performance by Spanwise Blowing over the Wing Leading Edge [PDF]
Spanwise blowing over the wing and canard of a 1:35 model of a close-coupled-canard fighter airplane configuration (similar to the Kfir-C2) was investigated experimentally in low-speed flow.
Salomon, M., Seginer, A.
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Rotor/wing aerodynamic interactions in hover [PDF]
An experimental and theoretical investigation of rotor/wing aerodynamic interactions in hover is described. The experimental investigation consisted of both a large-scale and small-scale test.
Felker, F. F., Light, J. S.
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Comparison of aerodynamic theory and experiment for jet-flap wings [PDF]
Aerodynamic theory predictions made for a jet flapped wing were compared with experimental data obtained in a fairly extensive series of tests in the Langley V/STOL tunnel. The tests were made on a straight, rectangular wing and investigated two types of
Gainer, T. G., Vogler, R. P., Yip, L. P.
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Journal of Mechanical EngineeringAn analysis of modern numerical methods for film cooling simulation on a flat surface, considering current CFD (Computational Fluid Dynamics) trends during 2019–2025, is presented in the paper. More than 25 recent studies devoted to 3D CFD simulations of
Oleh V. Shevchuk
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Wind tunnel studies of circulation control elliptical airfoils [PDF]
Effects of blown jets on the lift and drag of cambered elliptical airfoils are described. Performance changes due to a splitter plate attached to the lower surface of an elliptical airfoil near the trailing edge with and without blowing are indicated ...
Franke, M. E., Harvell, J. K.
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Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds [PDF]
A V/STOL tunnel study was performed to determine the effects of spanwise blowing on longitudinal aerodynamic characteristics of a model using a vectored-over-wing powered lift concept.
Leavitt, L. D., Yip, L. P.
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